# N427UP: 1992 Boeing 757-24APF

- Status: Valid registration
- Airframe: [Boeing 757-24APF](https://openairdocs.org/model/boeing-757-24apf) (registry code 1384969, 178 seats)
- Engine: [Pratt & Whitney PW2040](https://openairdocs.org/engine/pratt-whitney-pw2040) (registry code 52121)
- Data sheets: [TCDS E17NE](https://openairdocs.org/tcds/E17NE) (Pratt & Whitney) (OpenAirDocs)
- Serial number: 25458
- Year built: 1992
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: September 3, 1992
- Certificate issued: September 17, 1992
- Expires: May 31, 2028
- Mode S code: A51770
- Registered owner: [United Parcel Service Co](https://openairdocs.org/faa-owner/UNITED%20PARCEL%20SERVICE%20CO)
- Location: [Louisville, KY](https://openairdocs.org/faa-place/KY/Louisville)
- Owner type: Corporation
- Owner's area on the map: 38.2585° N, 85.5398° W: Placed by OpenAirDocs at the center of ZIP code 40223, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=427UP
- Page: https://openairdocs.org/aircraft/N427UP

From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination.

## ADs that may apply (OpenAirDocs): 15 in force

### Matched by airframe (Boeing 757-24APF)

None in force.

### Matched by engine (Pratt & Whitney PW2040)

- [AD 2026-07-06](https://openairdocs.org/ad/2026-07-06): Turbine Section · Pratt & Whitney F117-PW-100, PW2037, PW2037D and 3 more. Effective May 29, 2026
- [AD 2024-12-04](https://openairdocs.org/ad/2024-12-04): Turbine Section · Pratt & Whitney PW2037, PW2037M and PW2040. Effective Aug 13, 2024
- [AD 2021-14-13](https://openairdocs.org/ad/2021-14-13): Turbine Section · Pratt & Whitney F117-PW-100, PW2037, PW2037M and 1 more. Effective Sep 1, 2021
- [AD 2019-05-01](https://openairdocs.org/ad/2019-05-01): Turbine/Turboprop Engine · Pratt & Whitney F117-PW-100, PW2037, PW2037D and 6 more. Effective Apr 16, 2019
- [AD 2018-22-06](https://openairdocs.org/ad/2018-22-06): Fuel Control/Turbine Engines · Pratt & Whitney PW2037, PW2037M and PW2040. Effective Dec 3, 2018
- [AD 2018-14-10](https://openairdocs.org/ad/2018-14-10): Fuel Control Turbine Engines · Pratt & Whitney PW2037, PW2037M and PW2040. Effective Sep 28, 2018
- [AD 2012-02-01](https://openairdocs.org/ad/2012-02-01): Fan blades · Pratt & Whitney Division PW2037, PW2037M and PW2040. Effective Apr 24, 2012
- [AD 2009-14-05](https://openairdocs.org/ad/2009-14-05): High-pressure compressor (HPC) · Pratt & Whitney Division PW2037, PW2037M and PW2040. Effective Jul 23, 2009
- [AD 2009-10-08](https://openairdocs.org/ad/2009-10-08): High-pressure turbine 2nd stage hubs that have previously been exposed to Pratt & Whitney cleaning procedure SPOP 10 or SPOP 9 or equivalent procedure. · Pratt & Whitney Division PW2037, PW2037M and PW2040. Effective Jun 17, 2009
- [AD 2007-02-06](https://openairdocs.org/ad/2007-02-06): High pressure compressor (HPC) drum rotor disk assemblies · Pratt & Whitney Division PW2037, PW2037M and PW2040. Effective Feb 28, 2007
- [AD 2005-18-03](https://openairdocs.org/ad/2005-18-03): Engine manufacturer's time limits section (TLS) · Pratt & Whitney Division PW2037, PW2037D, PW2037M and 5 more. Effective Feb 28, 2006
- [AD 99-20-03](https://openairdocs.org/ad/99-20-03): High Pressure Turbine Disks · Pratt & Whitney Division PW2037, PW2037M, PW2040 and 2 more. Effective Nov 23, 1999
- [AD 96-18-08 R1](https://openairdocs.org/ad/96-18-08-R1): (HPT) High Pressure or (LPT) Low Pressure Turbine · Pratt & Whitney Division PW2037, PW2037M, PW2040 and 2 more. Effective Nov 10, 1998
- [AD 97-11-51 R1](https://openairdocs.org/ad/97-11-51-R1): First Stage High Pressure Turbine (HPT) Disk Assembly · Pratt & Whitney Division PW2037, PW2037M, PW2040 and 5 more. Effective Aug 7, 1997
- [AD 88-03-52](https://openairdocs.org/ad/88-03-52): Fuel Quantity Indication System · Pratt & Whitney Division PW2037 and PW2040. Effective Jul 13, 1988

### Historical (superseded or no longer in force)

- [AD 2017-12-03](https://openairdocs.org/ad/2017-12-03) (historical): Fuel Control Turbine Engines · Pratt & Whitney PW2037, PW2037M and PW2040. Effective Jul 20, 2017
- [AD 2017-11-06](https://openairdocs.org/ad/2017-11-06) (historical): Turbine/ Turboprop Engine · Pratt & Whitney F117-PW-100, PW2037, PW2037D and 6 more. Effective Jul 18, 2017
- [AD 2014-05-32](https://openairdocs.org/ad/2014-05-32) (historical): Diffuser-to-high-pressure turbine (HPT) case flange · Pratt & Whitney F117-PW-100, PW2037, PW2037D and 8 more. Effective May 5, 2014
- [AD 2002-12-06](https://openairdocs.org/ad/2002-12-06) (historical): Time Limits Section (TLS) · Pratt & Whitney Division PW2037, PW2037M, PW2040 and 5 more. Effective Jul 17, 2002
- [AD 2000-21-09](https://openairdocs.org/ad/2000-21-09) (historical): Critical Life-limited Parts · Pratt & Whitney Division PW2037, PW2037M, PW2040 and 5 more. Effective Jan 22, 2001
- [AD 99-08-14](https://openairdocs.org/ad/99-08-14) (historical): Maintenance Program, Mandatory Inspections · Pratt & Whitney Division PW2037, PW2037M, PW2040 and 5 more. Effective May 13, 1999

## Information bulletins (advisory)

None matched.

## NTSB investigations

None matched to N427UP.

## FAA accident and incident reports (2)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20130122001499I](https://openairdocs.org/incident/20130122001499I), Jan 22, 2013: Boeing 757-24APF (N427UP), Louisville, KY, No damage. Short final at 2000 with aircraft fully configured flying visual approach with auto throttles on, aircraft suddenly pitched up and trim seemed to runaway.…
- [Incident 19960806030339I](https://openairdocs.org/incident/19960806030339I), Aug 6, 1996: Boeing 75724APF (N427UP), Louisville, KY, Minor damage. Narrative: during a maintenance procedure, a counter-balance weight was loaded on this aircraft. The counter-balance was not removed after the maintenance was…

## Service difficulty reports (229, newest 50)

As reported by operators and repair stations. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR IPXA2026030476823](https://openairdocs.org/sdr/IPXA2026030476823), Feb 12, 2026: SKIN. DAMAGED. MAJOR REPAIR, UPPER FUSELAGE EXTERNAL SKIN AT BS 1370, S4L - S5L HAD A LIGHTNING STRIKE. TEMPORARY FASTENER INSTALLED. REMOVED FASTENER IN FUSELAGE FOR LIGTHNIN
- [SDR IPXA2026022820240](https://openairdocs.org/sdr/IPXA2026022820240), Feb 9, 2026: TEE FITTING. CORRODED. LOWER FUSELAGE BS 1220 LT SIDE TEE FITTING EXFOLIATED. INSTALLED A NEW TEE FITTING IAW SRM 51-40-02.
- [SDR IPXA2026030320044](https://openairdocs.org/sdr/IPXA2026030320044), Feb 9, 2026: TEE ANGLE. CORRODED. RIGHT FUSELAGE BS 1147 TEE ANGLE GOUGED AND CORRODED. INSTALLED A NEW TEE ANGLE, TWO STRAPS, & ONE ANGLE IAW SRM 51-40-02.
- [SDR IPXA2026030320240](https://openairdocs.org/sdr/IPXA2026030320240), Feb 9, 2026: TEE ANGLE. CORRODED. LOWER FUSELAGE BS 1220, LT SIDE TEE ANGLE EXFOLIATED.
- [SDR IPXA2026022786894](https://openairdocs.org/sdr/IPXA2026022786894), Feb 7, 2026: SKIN. DELAMINATED. MAJOR REPAIR, APU COMPT LOWER SKIN BELOW THE EXHAUST DUCT INNER SURFACE DELAMINATED AT BS 1992. THE PROTECTIVE COATING WAS RESTORED IAW AMM 51-21-15-370-802.
- [SDR IPXA2026022486878](https://openairdocs.org/sdr/IPXA2026022486878), Feb 7, 2026: SKIN. DELAMINATED. MAJOR REPAIR APU COMPT LH WALL INNER SKIN DELAMINATED IN AREA ABOVE THE OIL COOLER AIR EXIT DUCT. PREPARED AREA AND FABRICATED REPAIR PARTS IAW B757-200PF SRM 5
- [SDR IPXA2026030387426](https://openairdocs.org/sdr/IPXA2026030387426), Feb 7, 2026: BRACKET. CRACKED. LEFT MLG WW INBD SEAL RETAINER SUPPORT STRUCTURE BRACKET 6EA, FOUND CRACKED AFTER REMOVAL OF SEAL RETAINER BS 1060. INSTALLED NEW BRACKETS IAW SRM 51-40-02.
- [SDR IPXA2026022593920](https://openairdocs.org/sdr/IPXA2026022593920), Feb 7, 2026: SUPPORT ANGLE. CORRODED. FWD CARGO AT STA 863 BULKHEAD PANEL SUPPORT ANGLE LBL 19 - RBL 19 HAS CORROSION DOT 5842-11 REMOVED CORROSION AT THE STA 863 BULKHEAD PANEL SUPPORT ANGLE LBL 19
- [SDR IPXA2026021691664](https://openairdocs.org/sdr/IPXA2026021691664), Feb 7, 2026: TRANSITION PANEL. DENTED. FWD CARGO TRANSITION PANEL AT STA 630 RBL 22 HAS A GOUGE. REMOVED DAMAGE SECTION OF WEB (SIDE PANEL). IAW WITH SREO-3220-REQ003 AND SRM 51-70-13 STEP 1. INSTALL
- [SDR IPXA2026030267696](https://openairdocs.org/sdr/IPXA2026030267696), Feb 6, 2026: BRACKET. CORRODED. ACCESS DOOR 313AL LT & RT LATCH STOPS AT THE CUT-OUT, TWO BRACKETS ARE CORRODED. REMOVED ADJACENT STRIP AT BS 1885 TO FACILTATE MAINTENANCE, FOR REMOVAL OF ACCE
- [SDR IPXA2026021468498](https://openairdocs.org/sdr/IPXA2026021468498), Feb 6, 2026: STRAP. CORRODED. APU INLET DOOR FWD OF OPENING HAS CORROSION. REMOVED STRAP IAW SRM 51-40-02. INSTALLED NEW STRAP IAW SRM 51-40-02 IN APU INLET DOOR FWD.
- [SDR IPXA2026030360879](https://openairdocs.org/sdr/IPXA2026030360879), Feb 5, 2026: INTERCOSTAL. CORRODED. RIGHT WING TO BODY INTERCOSTAL, BS 1040 - 1060, RBL 60 CORRODED. INSTALLED A NEW INTERCOSTAL IAW SRM 51-40-02-0G.
- [SDR IPXA2026030359670](https://openairdocs.org/sdr/IPXA2026030359670), Feb 5, 2026: TEE ANGLE. CORRODED. RIGHT WING TO BODY TEE ANGLE AT BS 1040 - 1059, RBL 40, INLET STRUCTURE CORRODED.
- [SDR IPXA2026022760898](https://openairdocs.org/sdr/IPXA2026022760898), Feb 5, 2026: INTERCOSTAL. CORRODED. RIGHT WING TO BODY INTERCOSTAL, BS 1040.2, RBL 40 - 60 CORRODED. INSTALLED A NEW INTERCOSTAL IAW SRM 51-40-02-OG.
- [SDR IPXA2026022860882](https://openairdocs.org/sdr/IPXA2026022860882), Feb 5, 2026: INTERCOSTAL. CORRODED. RIGHT WING TO BODY INTERCOSTAL AT BS 1040 - 1060, RBL 65 CORRODED. APPLICATION OF CIC ON INTERCOSTAL.
- [SDR IPXA2026030360752](https://openairdocs.org/sdr/IPXA2026030360752), Feb 5, 2026: TEE ANGLE. CORRODED. LEFT WING TO BODY, BS 1030 BEHIND PANEL 197AL TEE ANGLE CORRODED AT LBL 26. INSTALLED A NEW TEE ANGLE IAW SRM 51-40-02.
- [SDR IPXA2026021961043](https://openairdocs.org/sdr/IPXA2026021961043), Feb 5, 2026: SHIM. CORRODED. FAULT/STR/ZONE 100 EXTERIOR RIGHT SIDE. WINGB / BODY PANEL 198KR STRUCTURE HAS CORROSION. REMOVED 01 EA SHIM LOCATED BTW STA 1180 TO STA 1240 AND RBL57. IAW B75
- [SDR IPXA2026030841896](https://openairdocs.org/sdr/IPXA2026030841896), Feb 4, 2026: TEE ANGLE. CORRODED. RIGHT WING TO BODY TEE ANGLE AT BS 1060, RBL 10 - 40 HAS CORROSION AT NUTPLATE HOLES. INSTALLED TEE-ANGLE AND PLATES AT RT WING TO BODY IAW SRM 51-40-02.
- [SDR IPXA2026030243996](https://openairdocs.org/sdr/IPXA2026030243996), Feb 4, 2026: PANEL. CRACKED. NR 2 PYLON GAP PANEL HAS A CRACK IN LOWER SURFACE. INSTALLED ONE DOUBLER & FILLER WASHERS IAW SRM 51-40-02, AND SRM 57-41-01-2R-3, REPAIR 3.
- [SDR IPXA2026022839378](https://openairdocs.org/sdr/IPXA2026022839378), Feb 4, 2026: FRAME. DENTED. AFT CARGO FRAME AT BS 1500 RT, DENTED. VERIFIED ACCOMPLISHMENT OF EO-96676-REQ1, AND EA 757-5360-27-A4324, REV- AS RII IAW UPS GMM 04-02-01-15.
- [SDR IPXA2026030443086](https://openairdocs.org/sdr/IPXA2026030443086), Feb 4, 2026: TEE FITTING. GOUGED. FAULT - STR - Z100 - LH UPPER WING TO BODY T-CHORD AT STA 1147 HAS GOUGE ON EDGE DOT 5698-08 INSTALLED T-CHORD AT LH WING STA 1147 I.A.W. B757 SRM 51-40-02.
- [SDR IPXA2026020942975](https://openairdocs.org/sdr/IPXA2026020942975), Feb 4, 2026: SUPPORT. CRACKED. LEFT MLG I/B SEAL RETAINER SUPPORT STRUCTURE HAS A CRACK IN THE CORNER AT BS 1060 VERIFIED INSTALLED SEAL RETAINER SUPPORT STRUCTURE AT LT MLG INBD BS 1060 IAW 
- [SDR IPXA2026022139192](https://openairdocs.org/sdr/IPXA2026022139192), Feb 4, 2026: FRAME. DENTED. MAJOR REPAIR, AFT CARGO FRAME AT STA 1300 RH IS DENTED. VERIFIED STEP 47. COMPLIED WITH EO-96677-REQ1, AND EA 757-5360-27-A4325, REV-.
- [SDR IPXA2026030342999](https://openairdocs.org/sdr/IPXA2026030342999), Feb 4, 2026: TEE ANGLE. CORRODED. LEFT WING TO BODY TEE ANGLE, BS 1260, BEHIND PANEL 197LL, CORRODED.
- [SDR IPXA2026030340724](https://openairdocs.org/sdr/IPXA2026030340724), Feb 4, 2026: TEE ANGLE. CORRODED. LEFT WING UNDER UPPER WING TO BODY PANEL 195BL HAD CORROSION. INSTALLED A TEE ANGLE IAW SRM 51-40-02.
- [SDR IPXA2026030341147](https://openairdocs.org/sdr/IPXA2026030341147), Feb 4, 2026: DOUBLER. CORRODED. RIGHT WING TO BODY TEE ANGLE, BS 1040 - 1059, RBL 40 - 60, INLET STRUCTURE HAD CORROSION. INSTALLED RAMP EXHAUST DOUBLER & PAX EXHAUST ASSY AT RT WING TO BODY T
- [SDR IPXA2025120140366](https://openairdocs.org/sdr/IPXA2025120140366), Nov 25, 2025: DOOR SEAL. TORN. CREW ENTRY DOOR SEAL TORN (FAA FINDING). TRIM ENTRY DOOR SEAL TO CLEAR DOOR LATCH MECHANISM IAW DWG 232N1643 SH3. OPS CHECKED NORMAL.
- [SDR IPXA2025112640366](https://openairdocs.org/sdr/IPXA2025112640366), Nov 25, 2025: DOOR SEAL. TORN. CREW ENTRY DOOR SEAL TORN.
- [SDR IPXA2025022044028](https://openairdocs.org/sdr/IPXA2025022044028), Feb 19, 2025: LEVER. BINDING. CAPTAINS WINDOW UNLOCK LEVER HARD TO MOVE. ACCOMPLISHED ADJUSTMENT OF N2 WINDOW IAW AMM 56-11-02-825-001 REV 136. OPERATIONAL TEST IAW AMM 56-11-02-715-020 REV 
- [SDR IPXA2025011305368](https://openairdocs.org/sdr/IPXA2025011305368), Jan 3, 2025: WINDOW. FAULTED. L SIDE WINDOW *EICAS. LH NO.2 SLINGING WINDOW REPLACED BY SERVICEABLE. I.A.W AMM 56-11-02/401 REV 135, CONFIRM THE WINDOW IS CORRECT ELECTRICAL CONNECTED IAW GM
- [SDR IPXA2025010305368](https://openairdocs.org/sdr/IPXA2025010305368), Jan 3, 2025: CONTROLLER. MALFUNCTIONED. *SDR FILED OPEN* L SIDE WINDOW *EICAS( ACCOMPLISHED TROUBLESHOOTING PER WDM 30-41-12-1 REV 97. SWAPPED WINDOW HEAT CONTROLLER LEFT WITH RIGHT. SAME FAULT. SWAPP
- [SDR IPXA202410290001](https://openairdocs.org/sdr/IPXA202410290001), Oct 15, 2024: O-RING. DEFORMED. LOST THE LEFT HYD ALMOST COMPLETELY DURING DESCENT TO LHBP (BUDAPEST, LISZT FERENC NATIONAL AIRPORT HUNGARY). THE A/C LANDED AND STOPPED SAFELY ON RNWY 13R. A/C
- [SDR IPXA2024101636812](https://openairdocs.org/sdr/IPXA2024101636812), Oct 15, 2024: PACKING. LEAKING. *EMERGENCY DECLARED* L HYD SYS PRESS PERFORMED QRH PROCEDURES ENG 1 CASE DRAIN MODULE UNION AND PACKING REPLACED IAW AMM 29-11-17 ,LEAKAGE CHECK SATIS,IAW AMM 2
- [SDR IPXA2024031116195](https://openairdocs.org/sdr/IPXA2024031116195), Feb 29, 2024: INTERCOSTAL. CORRODED. *SDR FILED OPEN* FAULT: L/H FWD OF HOT AIR EXHAUST HAS CORROSION. DOT 33-007 INSTALLED NEW INTERCOSTAL IAW B757 SRM 51-40-02-0G. INSTALLED HOT AIR EXHAUST L/H C
- [SDR IPXA2024031805314](https://openairdocs.org/sdr/IPXA2024031805314), Feb 28, 2024: FLOORBEAM. CORRODED. FLOORBEAM BS 1040 BETWEEN LBL 10 TO LBL 20 LOWER SURFACE WITH CHAFING INSTALLED T-CHORD STA 1040 I.A.W. B757 SRM 51-40-02-OG. JOB WAS ACCOMPLISHED PER UPS EO: E
- [SDR IPXA2024031405260](https://openairdocs.org/sdr/IPXA2024031405260), Feb 28, 2024: FLOORBEAM. CORRODED. FAULT- T-CHORD STA 900 BETWEEN LBL 20 TO LBL 40 LOWER SURFACE WITH CHAFING. INSTALLED T-CHORD AND (8 EA) REPAIR SPLICE PLATES I.A.W. B757-200 SRM 51-40-02-0G AN
- [SDR IPXA2024031405314](https://openairdocs.org/sdr/IPXA2024031405314), Feb 28, 2024: FLOORBEAM. CHAFED. T-CHORD STA 1040 BETWEEN LBL 10 TO LBL 20 LOWER SURFACE WITH CHAFING VERIFIED ACCOMPLISHMENT OF EA 757-5340-27-A3538 STEPS 1-3 PRELIMINARY 1
- [SDR IPXA2024031406476](https://openairdocs.org/sdr/IPXA2024031406476), Feb 28, 2024: FRAME. DENTED. AFT CARGO PIT STA 1320, SRG 26 RH HAS A DENT ON FRAME ACCOMPLISH REPAIR PER EO-89673-REQ1 REV 1 AND VT-MAE EA 757-5360-27-A3530, REV. -., PRIOR TO FURTHER FLIGH
- [SDR IPXA2024031306423](https://openairdocs.org/sdr/IPXA2024031306423), Feb 28, 2024: SHEAR TIE. DENTED. AFT CARGO PIT STA 1320, STG 25 LH HAS A DENT ON FRAME. VERIFIED ACCOMPLISMENT OF STEPS 12-27 OF EA 77-5360-27-A3533 REV. WITH NOTED DEVIATION.
- [SDR IPXA2024031204950](https://openairdocs.org/sdr/IPXA2024031204950), Feb 28, 2024: TEE FITTING. CORRODED. *SDR FILED OPEN* FAULT - T-CHORD STA 1040 BETWEEN RBL 10 TO RBL 20 LOWER SURFACE WITH CHAFING. VERIFIED: INSTALLED T-CHORD STA 1040 I.A.W. B757 200 51-40-02-OG.
- [SDR IPXA2024031371410](https://openairdocs.org/sdr/IPXA2024031371410), Feb 26, 2024: TRANSITION PANEL. CORRODED. AFT CARGO PIT - RH SIDE TRANSITION PANEL HAS EXFOLIATION CORROSION ARROUND TIE DOWN FITTINGS AT STA 1620, 1600 AND 1580 INSTALLED DOUBLER AND TRANSITION PANEL I
- [SDR IPXA2024031371207](https://openairdocs.org/sdr/IPXA2024031371207), Feb 26, 2024: TRANSITION PANEL. CORRODED. AFT CARGO PIT - RH SIDE TRANSITION PANEL BETWEEN STA 1360 AND 1380 HAS EXFOLIATION CORROSION. INSTALLED TRANSITION PANEL BTW STA 1360 AND 1380 RH IAW SRM 51-40-
- [SDR IPXA2024030471433](https://openairdocs.org/sdr/IPXA2024030471433), Feb 26, 2024: TIE DOWN. CORRODED. FAULT: AFT CARGO PIT - TIE DOWN FITTING STA 1500 RH SIDE WITH EXFOLIATION CORROSION INSTALLED TIE DOWN FITTING P/N 146N5440-56 BATCH 4245698 AT STA 1500 RH IAW 
- [SDR IPXA2024022771207](https://openairdocs.org/sdr/IPXA2024022771207), Feb 26, 2024: TRANSITION PANEL. CORRODED. AFT CARGO PIT - RH SIDE TRANSITION PANEL BETWEEN STA 1360 AND 1380 HAS EXFOLIATION CORROSION. REMOVED TRANSITION PANEL BETWEEN STA 1310 TO STA 1380 R/H SIDE I.A
- [SDR IPXA2024022771410](https://openairdocs.org/sdr/IPXA2024022771410), Feb 26, 2024: TRANSITION PANEL. CORRODED. *** SDR FILED OPEN *** FAULT: AFT CARGO PIT - RH SIDE TRANSITION PANEL HAS EXFOLIATION CORROSION ARROUND TIE DOWN FITTINGS AT STA 1620, 1600 AND 1580 REMOVED CO
- [SDR IPXA2023121901449](https://openairdocs.org/sdr/IPXA2023121901449), Dec 19, 2023: UNKNOWN. UNKNOWN. *** DIVERSION *** AT APPROX V/R CAPT PFD DISPLAYED WINDSHEAR WITH FULL SCALE A/S AND ALT DEVIATIONS OVERSPEED, RUDDER RATIO AND MACH SPEED TRIM EICAS ILLUMINATE
- [SDR IPXA2023051293198](https://openairdocs.org/sdr/IPXA2023051293198), May 11, 2023: ENGINE. FIRE. INSPECTION TYPE:NAR- ENG FIRE ON GRND. SECURED ENG. 1 BOTTLE FIRED *DOES NOT MEET SDR CRITERIA*PCMCIA CARD DOWNLOADED AND RE-INSTALLED IAW AMM 31-31-90-401. ENG
- [SDR IPXA2022040380790](https://openairdocs.org/sdr/IPXA2022040380790), Apr 3, 2022: SPLICE STRAP. CORRODED. INSPECTION TYPE:S-4AFT CARGO SHEAR TIE AND BUTT SPLICE BEAR STRAP AT STA 1400, BETWEEN S-30R AND S-29L HAS CORROSIONREPAIRED IAW UPS EO B757-5330-83317-A AND VT
- [SDR IPXA2022032480445](https://openairdocs.org/sdr/IPXA2022032480445), Mar 24, 2022: FLOOR PANEL. DAMAGED. INSPECTION TYPE:INTMAIN CARGO COMPARTMENT, FLOOR PANEL 232XSF DAMAGEDFABBED PANEL 232XSF FROM 5024N400001SS-G, BATCH # 3855547 PER SREO B757-5320-9692-K
- [SDR 145Y20200707001](https://openairdocs.org/sdr/145Y20200707001), Jul 2, 2020: UNION. SHEARED. ENGINEER REPORTED AN OCCURRENCE FROM THE STATION PRG. OCCURRED AT 02.07.2020 AND WAS REPORTED AT 06.07.2020 TO HEALTH AND SAFETY DEPARTMENT QA/H&S NAYAK AIRCRAF

All 229: https://openairdocs.org/aircraft/N427UP/reports.md

## STCs that may be installed (OpenAirDocs)

None matched to this aircraft's models.

## Related

- Other Boeing 757-24APF aircraft: https://openairdocs.org/model/boeing-757-24apf/aircraft.md
- The Pratt & Whitney PW2040 engine: https://openairdocs.org/engine/pratt-whitney-pw2040.md

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